Talks and Poster Presentations (with Proceedings-Entry):
A. Steindl, A. Schirrer, S. Jakubek:
"Optimal Control for a Space Rendezvous";
Talk: 4th International Workshop on Advanced Dynamics and Model Based Control of Structures and Machines,
JKU Linz;
2019-09-22
- 2019-09-25; in: "Dynamics and Control of Advanced Structures and Machines",
H Irschik, M. Krommer, V. Matveenko, A. Belyaev (ed.);
Advanced Structured Materials/Springer, Cham,
156
(2019),
ISBN: 978-3-030-79324-1;
243
- 256.
English abstract:
We consider the transfer of a chaser vehicle to a space station using impulsive control with minimal fuel consumption. It is assumed that the space station moves on a circular Keplerian orbit in a rotational symmetric gravitational field and that the chaser vehicle has already reached the station´s orbital plane. The vehicle is steered by impulsive burns of the rockets. The problem is solved numerically using Pontryagin´s maximum principle for impulsive controls by a multiple shooting method and a continuation procedure to study the variation of the optimal control strategy for varying time constraints. The problem is studied using a local linearized system and the fully nonlinear system using local Cartesian and polar coordinates.
"Official" electronic version of the publication (accessed through its Digital Object Identifier - DOI)
http://dx.doi.org/10.1007/978-3-030-79325-8_21
Electronic version of the publication:
https://doi.org/10.1007/978-3-030-79325-8_21
Created from the Publication Database of the Vienna University of Technology.